This is an example from F900EX Sn 001.

 

 

 

 

 

Hector -in class with scott.

Jean-

Edgar –

Louis DOM Mnaviation

Miguel 2nd guy in my class.

Peachy -beard

 

 

 

Incoming Avionics issues:

WR works great over water.  Over land shows lots of returns.  GCS, Check tilt.

 

#3FMS ACARS FAIL.

NEW OCT 10, EID blank. Verfied, blank.

 

Irs 3 bad. Verifided, stays in 3 min to align.

Fms 1 SINGLE operation. Not verified. They are working fine.  Custom DB

VHF 2 xmit only 2 seconds. Verified

MFD has stayed black sometimes. From Devin. Verfied dead. Sg switching works.

Satfone inop.

CPDLC freezes, kusa, tail, tail, then sending. Air or ground. Idendify CB. 1OF 5 flight.

Pax brief inop.  Check moving map. Incydink dead

Bulbs interior. Measure for LED.

incoming airframe issues:

Number 3 throttles stiff

Hp bleed overheat , was number 3, now number 1. Old squawk.

Steering servo leak.

Copilot ws leaks at top.

DC4 at towing disc

Uplock roller dont roll.

Nose boot

RH  slat droop after 24 hours.

ICS audio scratchy. Verfied  Mic jack scratchy. Needs clean up.

ESSPRESSO maker inop.

Condensation in cabin when gnd apu run. Verified, check sock

DV window ai inop. Center window seems to accuulate ice.

Fwd galley water heater inop. Check sw.

CABIN TEMP  both only work in manual.  Verfied pax fail.  Pax motor failed

Glue for studs,

All the way to hot or cold.

Door seal whines lower portion.

APU GEN 10 amps low.

 

DV window brown at the edge

Foam at AOA covers

 

Fwd galley hand basin drain not connected.  Missing hardware

………….

BEACON voltage

 

Good afternoon.

We are trying  to ping test beacon pn 266-e5542-00.  Falcon airframe work card does not give the acceptable voltage on the end terminal.

Can yougive us some guidance?

Todd

Good morning, Todd,

The battery Min Acceptable voltage is 2.97V.

 

I hope this helps.

Best Regards

Samir Purohit

Business Development Manager – Dukane Seacom Inc./ Radiant Power Corp.

(Cell)   +1   941-799-0061

Show quoted text

Thanks so much for the response.   Todd

 

 

 

 

 

 

 

 

 

 

 

 

Without  sb 329

Lw 7036 lbs

Rw 7080 lbs

Center 6884 lbs, you cannot jamb the center all the way full until the wing are End-of-fueling.

 

With sb 329

Lw 7006 lbs

Rw 7050 lbs

 

 

 

 

 

 

https://www.libertyjet.com/jet-ownership-costs.aspx?jetType=FALCON%20900

2023 , f900ex MSPGOLD 556/h / engine , 30k a month

 

There was a little controversy on weighing, here is how it played out:

 

 

 

here is the math

 

716BH WB calculation

 

 

 

27 lbs to close, only when upper trim is installed.

 

 

After 30 hours or so the top 5 inches of the seal blows out at ~ 9.3 psi.

 

 

 

 

 

 

 

 

Oxygen

 

 

 

 

 

 

 

 

 

 

Fwd of EID display

 

Main entry door

 

 

RH COAT CLOSET

 

 

 

 

 

 

 

Baggage fwd wall.

 

 

 

 

 

 

 

 

 

 

 

 

One half of 1 meter on climate control panel illuminates. You can press on the left half of the face, and it will come and go.

 

 

 

Scratches at flap handle

 

Lower left overhead panel inop

 

Pressirization computer lower left side light spill

 

#1 RTU upper rh corner light spill.

 

Both audio panels minor light spill all edges

1. 

Light spill at #3 IRU

No illumination on any keys at any of the 3 FMS controll heads

Placard brocken at horn silence

 

 

 

 

 

 

 

 

 

 

 

 

This is an old presentation i set up.

I thinkmi cabbaged some stuff from flcon, and added some art.

Old Auxilec presentation:
AuxilecStarterGeneratorOld

Old notes:

Old troubleshooting notes on a long-legged problem: engines running:

1.  Check for Bleed leak blowing on GCU.  BE very carefull if you elect to run the AI on the ground.  !!!!!!APU BLEED OFF!!!!!!, slats extended.    20 seconds ground test max. leave the slats out to cool.
2.  Test “E” ground quality.  Fluke on volts.  Black lead to airframe ground, red lead to GCU Black test point.  Very small voltage~ .1v.  less is better
3. Volt drop on line contractor.  Fluke meter on volts.  Red lead on upper contactor, bottom big bolt, black lead on same contactor, upper big bolt. Very small voltage~ .1v.  less is better.
4. Ripple test.  use fluke MIN/MAX.

Run each test with only 1 gen online, 50 to 100 amps load, try to hold conditions quite similar for each test.

some other thoughts:
look at big E terminal, small 20awg terminal.

double check each  GCU voltage. Is it stable at 28.5? is it stable with load? is it stable with RPM change?

select cockpit red switch to off.  Is the voltage of a running generator, cockpit switch selected off,  .7v to 1.0v at idle? this checks the quality of the permanent magnets inside the Generator.

ASSURE that NO ENGINE GENERATOR  has a cooling fan installed. (possibly a borescope through the black sooty outlet.) or it mat be necessary to unbolt the cooling exhaust.

Initial problem definition:

#3 Gen Light occasionally, Much troubleshooting. Gen 3 amps tend toward zero. #1 seems to “take the load”

 

History:

#3 gen troubleshooting, #1, #3 gen shunts…..?Removed?

Detailed summary of troubleshooting:

Customer_Invoice_-_Work_Order-_13548-05-2021